新型高速空天运输发射平台气动布局设计研究

The Aerodynamic Layout Study of a New High-speed Aircraft for Transporting and Launching Aerospace Vehicles

根据空天飞行器发展趋势,利用乘波体的高升阻比特点,提出了用于运输发射空天飞行器的新型高速空天运输发射平台,开展了气动布局设计,完成新型高速空天运输发射平台巡航状态下的气动数值模拟分析,分析结果表明文中所设计的新型高速空天运输发射平台气动性能优良,设计结论和分析方法可应用于新型高速空天发射平台工程设计。

According to the latest trends in aerospace vehicle development, employed the high lift-to-drag advantage of waverider, proposed a new high-speed aircraft for transporting and launching aerospace vehicles. The aerodynamic layout of the new high-speed aircraft was designed and the aerodynamic characteristics when the aircraft was cruising had been analyzed by numerical simulating. The results show that the aerodynamic performance is fine and satisfies the demands of the aircraft. The process and method can be applied to engineering design.